JP5485532B2 - 希釈および冷却が最適化された燃焼チャンバ壁およびそれを備えた燃焼チャンバおよびターボ機械 - Google Patents

希釈および冷却が最適化された燃焼チャンバ壁およびそれを備えた燃焼チャンバおよびターボ機械 Download PDF

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Publication number: JP5485532B2
Authority: JP; Japan
Prior art keywords: dilution; holes; diameter; combustion chamber; wall
Prior art date: 2007-10-22
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Active

Application number

JP2008270505A

Other languages

English (en)

Japanese (ja)

Other versions

JP2009103439A (ja

Inventor

ミシエル・ピエール・カザラン

パトリス・アンドレ・コマレ

ロマン・リユネル

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Safran Aircraft Engines SAS

Original Assignee

SNECMA SAS

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

2007-10-22

Filing date

2008-10-21

Publication date

2014-05-07

2008-10-21 Application filed by SNECMA SAS filed Critical SNECMA SAS

2009-05-14 Publication of JP2009103439A publication Critical patent/JP2009103439A/ja

2014-05-07 Application granted granted Critical

2014-05-07 Publication of JP5485532B2 publication Critical patent/JP5485532B2/ja

Status Active legal-status Critical Current

2028-10-21 Anticipated expiration legal-status Critical

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Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Turbine Rotor Nozzle Sealing (AREA)

JP2008270505A 2007-10-22 2008-10-21 希釈および冷却が最適化された燃焼チャンバ壁およびそれを備えた燃焼チャンバおよびターボ機械 Active JP5485532B2 (ja)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
FR0707360A FR2922630B1 (fr)	2007-10-22	2007-10-22	Paroi de chambre de combustion a dilution et refroidissement optimises,chambre de combustion et turbomachine en etant munies
FR0707360		2007-10-22

Publications (2)

Publication Number	Publication Date
JP2009103439A JP2009103439A (ja)	2009-05-14
JP5485532B2 true JP5485532B2 (ja)	2014-05-07

Family

ID=39529786

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
JP2008270505A Active JP5485532B2 (ja)	2007-10-22	2008-10-21	希釈および冷却が最適化された燃焼チャンバ壁およびそれを備えた燃焼チャンバおよびターボ機械

Country Status (6)

Country	Link
US (1)	US20090100839A1 (fr)
EP (1)	EP2053311B1 (fr)
JP (1)	JP5485532B2 (fr)
CA (1)	CA2642059C (fr)
FR (1)	FR2922630B1 (fr)
RU (1)	RU2478875C2 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2920032B1 (fr)	2007-08-13	2014-08-22	Snecma	Diffuseur d'une turbomachine
FR2922629B1 (fr) *	2007-10-22	2009-12-25	Snecma	Chambre de combustion a dilution optimisee et turbomachine en etant munie
FR2950415B1 (fr) *	2009-09-21	2011-10-14	Snecma	Chambre de combustion de turbomachine aeronautique avec trous de combustion decales ou de debits differents
FR2953907B1 (fr) *	2009-12-11	2012-11-02	Snecma	Chambre de combustion pour turbomachine
US10816202B2 (en)	2017-11-28	2020-10-27	General Electric Company	Combustor liner for a gas turbine engine and an associated method thereof
US11255543B2 (en)	2018-08-07	2022-02-22	General Electric Company	Dilution structure for gas turbine engine combustor
US11181269B2 (en)	2018-11-15	2021-11-23	General Electric Company	Involute trapped vortex combustor assembly
FR3095260B1 (fr) *	2019-04-18	2021-03-19	Safran Aircraft Engines	Procede de definition de trous de passage d’air a travers une paroi de chambre de combustion

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB1499950A (en) *	1975-08-25	1978-02-01	Caterpillar Tractor Co	Cooled gas turbine engine flame tube
DE3519938A1 (de) *	1985-06-04	1986-12-04	MTU Motoren- und Turbinen-Union München GmbH, 8000 München	Brennkammereinrichtung
FR2770283B1 (fr) *	1997-10-29	1999-11-19	Snecma	Chambre de combustion pour turbomachine
US6260359B1 (en) *	1999-11-01	2001-07-17	General Electric Company	Offset dilution combustor liner
RU2162194C1 (ru) *	1999-11-24	2001-01-20	Общество с ограниченной ответственностью Научно-производственное предприятие "ЭСТ"	Камера сгорания
US6408629B1 (en) *	2000-10-03	2002-06-25	General Electric Company	Combustor liner having preferentially angled cooling holes
US6543233B2 (en) *	2001-02-09	2003-04-08	General Electric Company	Slot cooled combustor liner
US6655146B2 (en) *	2001-07-31	2003-12-02	General Electric Company	Hybrid film cooled combustor liner
US6513331B1 (en) *	2001-08-21	2003-02-04	General Electric Company	Preferential multihole combustor liner
US7000400B2 (en) *	2004-03-17	2006-02-21	Honeywell International, Inc.	Temperature variance reduction using variable penetration dilution jets
FR2869094B1 (fr) *	2004-04-15	2006-07-21	Snecma Moteurs Sa	Chambre de combustion annulaire de turbomachine a bride interne de fixation amelioree
US7216485B2 (en) *	2004-09-03	2007-05-15	General Electric Company	Adjusting airflow in turbine component by depositing overlay metallic coating
US7614235B2 (en) *	2005-03-01	2009-11-10	United Technologies Corporation	Combustor cooling hole pattern
FR2892180B1 (fr) *	2005-10-18	2008-02-01	Snecma Sa	Amelioration des perfomances d'une chambre de combustion par multiperforation des parois

2007
- 2007-10-22 FR FR0707360A patent/FR2922630B1/fr active Active
2008
- 2008-10-20 EP EP08167047.3A patent/EP2053311B1/fr active Active
- 2008-10-21 CA CA2642059A patent/CA2642059C/fr active Active
- 2008-10-21 JP JP2008270505A patent/JP5485532B2/ja active Active
- 2008-10-21 RU RU2008141813/06A patent/RU2478875C2/ru active
- 2008-10-22 US US12/255,987 patent/US20090100839A1/en not_active Abandoned

Also Published As

Publication number	Publication date
CA2642059C (fr)	2015-12-29
US20090100839A1 (en)	2009-04-23
EP2053311A1 (fr)	2009-04-29
JP2009103439A (ja)	2009-05-14
RU2478875C2 (ru)	2013-04-10
EP2053311B1 (fr)	2016-04-06
FR2922630B1 (fr)	2015-11-13
CA2642059A1 (fr)	2009-04-22
RU2008141813A (ru)	2010-04-27
FR2922630A1 (fr)	2009-04-24

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Publication	Publication Date	Title
JP5485532B2 (ja)	2014-05-07	希釈および冷却が最適化された燃焼チャンバ壁およびそれを備えた燃焼チャンバおよびターボ機械
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